SG144713A1 - Augmentor - Google Patents
AugmentorInfo
- Publication number
- SG144713A1 SG144713A1 SG200402056-6A SG2004020566A SG144713A1 SG 144713 A1 SG144713 A1 SG 144713A1 SG 2004020566 A SG2004020566 A SG 2004020566A SG 144713 A1 SG144713 A1 SG 144713A1
- Authority
- SG
- Singapore
- Prior art keywords
- centerbody
- augmentor
- pilot fuel
- combustion products
- outlet
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
- F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
- F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
- Exhaust Gas After Treatment (AREA)
- Air Supply (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/426,671 US7093442B2 (en) | 2003-04-30 | 2003-04-30 | Augmentor |
Publications (1)
Publication Number | Publication Date |
---|---|
SG144713A1 true SG144713A1 (en) | 2008-08-28 |
Family
ID=32990420
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200402056-6A SG144713A1 (en) | 2003-04-30 | 2004-04-15 | Augmentor |
Country Status (13)
Country | Link |
---|---|
US (1) | US7093442B2 (fr) |
EP (1) | EP1473519A3 (fr) |
JP (1) | JP3974595B2 (fr) |
KR (1) | KR100610732B1 (fr) |
AU (1) | AU2004201209B2 (fr) |
CA (1) | CA2460659A1 (fr) |
DE (1) | DE04252295T1 (fr) |
IL (1) | IL161423A0 (fr) |
NO (1) | NO20041762L (fr) |
PL (1) | PL366887A1 (fr) |
SG (1) | SG144713A1 (fr) |
TR (1) | TR200500469T3 (fr) |
TW (1) | TWI238871B (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2866675B1 (fr) * | 2004-02-24 | 2008-05-16 | Snecma Moteurs | Procede d'amelioration des performances d'allumage de dispositif de post-combustion pour turboreacteur double flux et dispositif de post-combustion a performance d'allumage amelioree |
US6983601B2 (en) * | 2004-05-28 | 2006-01-10 | General Electric Company | Method and apparatus for gas turbine engines |
US7174704B2 (en) * | 2004-07-23 | 2007-02-13 | General Electric Company | Split shroud exhaust nozzle |
US7437876B2 (en) * | 2005-03-25 | 2008-10-21 | General Electric Company | Augmenter swirler pilot |
US7467518B1 (en) | 2006-01-12 | 2008-12-23 | General Electric Company | Externally fueled trapped vortex cavity augmentor |
US8402744B2 (en) * | 2008-03-22 | 2013-03-26 | Pratt & Whitney Rocketdyne, Inc. | Valve system for a gas turbine engine |
US8286416B2 (en) * | 2008-04-02 | 2012-10-16 | Pratt & Whitney Rocketdyne, Inc. | Valve system for a gas turbine engine |
US8240126B2 (en) * | 2008-03-22 | 2012-08-14 | Pratt & Whitney Rocketdyne, Inc. | Valve system for a gas turbine engine |
US8578716B2 (en) * | 2008-03-22 | 2013-11-12 | United Technologies Corporation | Valve system for a gas turbine engine |
US8209987B2 (en) * | 2008-11-26 | 2012-07-03 | United Technologies Corporation | Augmentor pilot |
US8534071B1 (en) | 2012-04-06 | 2013-09-17 | United Technologies Corporation | Engine hot section vane with tapered flame holder surface |
US9879862B2 (en) | 2013-03-08 | 2018-01-30 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine afterburner |
CN113280366B (zh) * | 2021-05-13 | 2022-09-27 | 中国航空发动机研究院 | 一种基于自激扫掠振荡燃油喷嘴的加力燃烧室结构 |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2693083A (en) * | 1951-03-26 | 1954-11-02 | Roy W Abbott | Combination flame-holder and fuel nozzle |
US2780915A (en) * | 1951-12-05 | 1957-02-12 | Solar Aircraft Co | Fuel distribution system for jet engine and afterburner |
US2880573A (en) * | 1952-08-27 | 1959-04-07 | Gen Motors Corp | Afterburner fuel injection system |
US2979899A (en) * | 1953-06-27 | 1961-04-18 | Snecma | Flame spreading device for combustion equipments |
US2978865A (en) * | 1956-02-06 | 1961-04-11 | Curtiss Wright Corp | Turbo fan exhaust mixing device |
US2880574A (en) * | 1956-05-18 | 1959-04-07 | Curtiss Wright Corp | By-pass turbo jet engine construction |
US2847821A (en) * | 1956-06-21 | 1958-08-19 | Westinghouse Electric Corp | Fuel ignition apparatus for an afterburner in the bypass duct of a turbojet engine |
US2910828A (en) * | 1956-08-24 | 1959-11-03 | United Aircraft Company | Convergent-divergent variable area propulsion nozzle |
US2929203A (en) * | 1956-08-31 | 1960-03-22 | Westinghouse Electric Corp | Afterburning bypass aviation turbojet engine |
US3075353A (en) * | 1959-08-19 | 1963-01-29 | Gen Electric | Supersonic combustion |
US3712062A (en) * | 1968-04-17 | 1973-01-23 | Gen Electric | Cooled augmentor liner |
GB1305887A (fr) * | 1971-07-01 | 1973-02-07 | ||
US3938328A (en) * | 1971-11-08 | 1976-02-17 | The Boeing Company | Multicycle engine |
US4069661A (en) * | 1975-06-02 | 1978-01-24 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Variable mixer propulsion cycle |
US4185461A (en) * | 1978-01-10 | 1980-01-29 | The United States Of America As Represented By The Secretary Of The Air Force | Turbojet engine with combustor bypass |
US5136840A (en) * | 1982-09-30 | 1992-08-11 | General Electric Company | Gas turbine engine actuation system |
US4798048A (en) * | 1987-12-21 | 1989-01-17 | United Technologies Corporation | Augmentor pilot |
US5099644A (en) * | 1990-04-04 | 1992-03-31 | General Electric Company | Lean staged combustion assembly |
US5385015A (en) * | 1993-07-02 | 1995-01-31 | United Technologies Corporation | Augmentor burner |
US5396761A (en) * | 1994-04-25 | 1995-03-14 | General Electric Company | Gas turbine engine ignition flameholder with internal impingement cooling |
US5685140A (en) * | 1995-06-21 | 1997-11-11 | United Technologies Corporation | Method for distributing fuel within an augmentor |
US5867980A (en) * | 1996-12-17 | 1999-02-09 | General Electric Company | Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and an afterburner |
US6125627A (en) * | 1998-08-11 | 2000-10-03 | Allison Advanced Development Company | Method and apparatus for spraying fuel within a gas turbine engine |
US6463739B1 (en) * | 2001-02-05 | 2002-10-15 | General Electric Company | Afterburner heat shield |
-
2003
- 2003-04-30 US US10/426,671 patent/US7093442B2/en not_active Expired - Lifetime
-
2004
- 2004-03-11 CA CA002460659A patent/CA2460659A1/fr not_active Abandoned
- 2004-03-17 TW TW093107094A patent/TWI238871B/zh active
- 2004-03-24 AU AU2004201209A patent/AU2004201209B2/en not_active Ceased
- 2004-04-02 PL PL04366887A patent/PL366887A1/xx not_active Application Discontinuation
- 2004-04-15 IL IL16142304A patent/IL161423A0/xx unknown
- 2004-04-15 SG SG200402056-6A patent/SG144713A1/en unknown
- 2004-04-16 KR KR1020040026022A patent/KR100610732B1/ko not_active IP Right Cessation
- 2004-04-19 TR TR2005/00469T patent/TR200500469T3/xx unknown
- 2004-04-19 EP EP04252295A patent/EP1473519A3/fr not_active Withdrawn
- 2004-04-19 DE DE04252295T patent/DE04252295T1/de active Pending
- 2004-04-28 JP JP2004132325A patent/JP3974595B2/ja not_active Expired - Fee Related
- 2004-04-29 NO NO20041762A patent/NO20041762L/no not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
TW200424435A (en) | 2004-11-16 |
AU2004201209B2 (en) | 2005-10-27 |
EP1473519A3 (fr) | 2007-04-11 |
PL366887A1 (en) | 2004-11-02 |
US20040216444A1 (en) | 2004-11-04 |
KR20040094313A (ko) | 2004-11-09 |
TR200500469T3 (tr) | 2005-04-21 |
IL161423A0 (en) | 2004-09-27 |
TWI238871B (en) | 2005-09-01 |
AU2004201209A1 (en) | 2004-11-18 |
KR100610732B1 (ko) | 2006-08-09 |
NO20041762L (no) | 2004-11-01 |
DE04252295T1 (de) | 2005-06-23 |
EP1473519A2 (fr) | 2004-11-03 |
JP3974595B2 (ja) | 2007-09-12 |
US7093442B2 (en) | 2006-08-22 |
JP2004332729A (ja) | 2004-11-25 |
CA2460659A1 (fr) | 2004-10-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1391657A3 (fr) | Chambre de combustion de turbine à gaz et son procédé de fonctionnement | |
SG128549A1 (en) | Augmentor fuel conduit bushing | |
SG144713A1 (en) | Augmentor | |
EP1371906A3 (fr) | Chemise tubulaire de chambre de combustion de turbine à gaz avec cavité pour la création de vortex piégés | |
DE502005001467D1 (de) | Betriebsverfahren für eine Feuerungsanlage | |
EP1978307A3 (fr) | Chambre de combustion de turbine à gaz | |
CA2516753C (fr) | Methodes et dispositif de reduction des emissions d'une turbine a gaz | |
SG128547A1 (en) | Augmentor spray bar mounting | |
EP1777459A3 (fr) | Chambre de combustion pour turbine à gaz | |
WO2008070210A3 (fr) | Injection de carburant pilote pour un moteur à rotor d'onde | |
EP0845634A3 (fr) | Chambre de combustion pour turbine à gaz et son procédé de fonctionnement | |
EP2206964A3 (fr) | Configurations d'injecteur de combustible pour injection tardive pauvre | |
EP0810405A3 (fr) | Chambre de combustion pour une turbine à gaz et sa méthode de travail | |
CA2452972A1 (fr) | Methodes et systeme de production de poussee pour turbine a gaz | |
EP1333228A3 (fr) | Procédé et appareillage pour la réduction des émissions de chambres de combustion | |
EP1193449A3 (fr) | Ensemble de vrilles annulaires | |
MY126891A (en) | Methods for reducing gas turbine engine emissions | |
JPS5741524A (en) | Combustion method of gas turbine and combustor for gas turbine | |
EP0800041A3 (fr) | Chambre de combusion de turbine à gaz | |
EP1310737A3 (fr) | Chambre de combustion par diffusion à faibles émissions de NOx pour turbines à gaz | |
CA2394694A1 (fr) | Tuyere pilote de chambre de combustion de turbine a gaz | |
WO2005028960A3 (fr) | Chambre de combustion pilote pour la stabilisation de la combustion dans des moteurs de turbines a gaz | |
IL160830A0 (en) | Augmentor | |
CN103727534A (zh) | 用于延迟贫油喷射燃烧器系统的空气管理装置以及输送空气流的方法 | |
CN202578943U (zh) | 一种脉冲爆震发动机射流点火装置 |